Aircraft composites assessment by means of transient thermal NDT
By Nicolas P. Avdelidis, D. Almond, A. Dobbinson, B. Hawtin, Clemente Ibarra-Castanedo, Xavier P. V. Maldague. 2004
209 citations recorded by the source corpus.
Subfields: Biomedical Engineering, Civil and Structural Engineering, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/ff75cce4f48da49995db434a169144e5f9c02ae8
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Biomedical Engineering
In Civil and Structural Engineering
- Andrzej Katunin
- Thomas Blumensath
- Michal Dziendzikowski
- Richard P. Boardman
- Ander Biguri
- Hossein Towsyfyan
- Krzysztof Dragan
In Mechanics of Materials
- Laura Vega
- L. Toubal
- Andrzej Katunin
- Thomas Blumensath
- Francisco G. Bulnes
- Julio Molleda
- Michal Dziendzikowski
- Moussa Karama
Citations in the corpus
- Damage evolution and infrared thermography in woven composite laminates under fatigue loading (2006, background): “Fatigue damage in polymer composites has been extensively investigated [1–7].”
- Advances in applications of Non-Destructive Testing (NDT): A review (2021, background): “[43] presents the applications of transient thermal NDT in assessing the aircraft composites.”
- Successes and challenges in non-destructive testing of aircraft composite structures (2020, methodology): “Avdelidis et al.(159) applied pulsed IRT to CFRP laminates as well as honeycomb and sandwich structures and reported that real-time monitoring of all features was obtained using pulsed thermograph.”
- Infrared Thermography for Temperature Measurement and Non-Destructive Testing (2014, methodology): “Thermal images of defects in drilled holes (frame with permission from [144]).”
- Damage identification in aircraft composite structures: A case study using various non-destructive testing techniques (2015, methodology): “The authors of [12] presented the results of damage detection and localization (notches, delaminations and drilling defects) in aircraft composite structures using the transient thermography approach.”